BACKGROUND OF THE INVENTION
1. Field of the Invention
[0001] The present invention relates to a high-strength spring steel used in automobiles,
aircraft equipment, various types of industrial machinery, and so forth.
2. Description of the Related Art
[0002] In an effort to improve fuel economy, there has been an urgent need in recent years
for weight reductions in automobiles. These reductions are required of many different
parts, with suspension parts being no exception. One way of handling this is to set
a higher design stress for suspension springs. Specifically, it is effective to increase
the strength of springs. Si-Mn-based SUP7 and Si-Cr-based SUP12 are the main types
of suspension spring steel in use at the present time, but further increases in design
stress will require higher strength than with these types of steel. The strength of
a steel material is generally closely related to its hardness, but there was concern
that increasing the hardness of spring steel would lower its toughness. Specifically,
diminished toughness was an inevitable consequence of achieving hardness over that
of current spring steel. In increasing the strength of suspension springs, toughness
also had to be greater than that of current steel to ensure reliability in these springs.
SUMMARY OF THE INVENTION
[0003] In view of this, it is an object of the present invention to obtain a spring steel
that is harder than at present and that is also tougher than at present.
[0004] As a result of examining the effect of various elements on the hardness and toughness
of steel, the inventors learned that a high-strength spring steel combining both hardness
and toughness can be obtained by adjusting the proportions of its various elements.
[0005] Specifically, the present invention is a high-strength spring steel having a hardness
Hv of at least 600 upon tempered at 350°C after quenching, and an impact strength
of at least 40 J/cm
2, comprising 0.40 to 0.70 wt. % carbon, 1.00 to 2.50 wt. % silicon, 0.30 to 0.90 wt.
% manganese, 0.50 to 1.50 wt. % nickel, 1.00 to 2.00 wt. % chromium, 0.30 to 0.60
wt. % molybdenum, 0.25 to 0.50 wt. % copper, 0.01 to 0.50 wt. % vanadium, 0.010 to
0.050 wt. % niobium, 0.005 to 0.050 wt. % aluminum, 0.0045 to 0.0100 wt. % nitrogen,
0.005 to 0.050 wt. % titanium, and 0.0005 to 0.0060 wt. % boron, with phosphorus limited
to 0.010 wt. % or less, sulfur to 0.010 wt. % or less, and O
T to 0.0015 wt. % or less, and the remainder being composed of iron and unavoidable
impurities.
[0006] The reasons for limiting the components in the present invention are as follows.
[0007] Carbon: Carbon is an element that is effective at increasing strength, but the strength
required of spring steel cannot be obtained at less than 0.40 wt. %, and the spring
will be too brittle if the content exceeds 0.70 wt. %, so the content range was set
at 0.40 to 0.70 wt. %.
[0008] Silicon: Silicon is an element that is effective at increasing the strength of steel
through solid solution in ferrite, but a spring will not have satisfactory resistance
to permanent set in fatigue at a content of less than 1.00 wt. %, and if the content
exceeds 2.50 wt. %, then decarburization of the surface will tend to occur in the
hot forming of the spring, and there will be an adverse effect on the durability of
the spring, so the content range was set at 1.00 to 2.50 wt. %.
[0009] Manganese: Manganese is an element that is effective at enhancing the hardenability
of steel, and the content must be at least 0.30 wt. %, but exceeding 0.90 wt. % will
hamper toughness, so the content range was set at 0.30 to 0.90 wt. %.
[0010] Nickel: Nickel is an element that is effective at enhancing the hardenability of
steel, and the content must be at least 0.50 wt. %, but if the content exceeds 1.50
wt. %, residual austenite will increase and there will be an adverse effect on the
fatigue strength of the spring, so the content range was set at 0.50 to 1.50 wt. %.
[0011] Chromium: Chromium is an element that is effective at increasing the strength of
steel, but the strength required of a spring cannot be obtained at less than 1.00
wt. %, and toughness will be inferior if the content exceeds 2.00 wt. %, so the content
range was set at 1.00 to 2.00 wt. %.
[0012] Molybdenum: Molybdenum is an element that ensures hardenability and raises the strength
and toughness of steel, but these effects cannot be fully anticipated at less than
0.30 wt. %, and no further benefit will be derived from exceeding 0.60 wt. %, so the
content range was set at 0.30 to 0.60 wt. %.
[0013] Copper: Copper is an element that boosts corrosion resistance, but this effect will
not be realized at less than 0.25 wt. %, and exceeding 0.50 wt. % causes problems
such as cracking during hot rolling, so the content range was set at 0.25 to 0.50
wt. %.
[0014] Vanadium: Vanadium is an element that raises the strength of steel, but this effect
cannot be fully anticipated at less than 0.01 wt. %, and if 0.50 wt. % is exceeded,
carbides that do not dissolve in austenite will increase and compromise the spring
characteristics, so the content range was set at 0.01 to 0.50 wt. %.
[0015] Niobium: Niobium is an element that increases the strength and toughness of steel
through the precipitation of fine carbides and making the grains finer, but these
effects cannot be fully anticipated at a content of less than 0.010 wt. %, and if
the content exceeds 0.50 wt. %, carbides that do not dissolve in austenite will increase
and compromise the spring characteristics, so the content range was set at 0.010 to
0.050 wt. %.
[0016] Aluminum: Aluminum is an element that is required as a deoxidant and in order to
achieve the adjustment of austenite grain size, but the grains will not become finer
at a content of less than 0.005 wt. %, whereas castability will tend to suffer if
0.050 wt. % is exceeded, so the range was set at 0.005 to 0.050 wt. %.
[0017] Nitrogen: Nitrogen is an element that bonds with aluminum and niobium to form AlN
and NbN, serving to reduce the austenite grain size, and through this grain-refining,
helps to increase toughness. For this effect to be realized, the content must be at
least 0.0045 wt. %. However, nitrogen should be added to keep the amount as small
as possible in order to achieve better hardenability by addition of boron, and excessive
addition of nitrogen leads to foaming on the ingot surface during solidification and
makes it more difficult to cast the steel. To avoid this, the upper limit must be
set at 0.0100 wt. %. Therefore, the amount of nitrogen addition was set at 0.0045
to 0.0100 wt. %.
[0018] Titanium: Nitrogen in steel bonds with the boron discussed below and forms BN which
will cause deterioration of the effect of boron on enhancing hardenability. Titanium
is added to prevent such deterioration. Its effect cannot be fully anticipated at
a content of less than 0.005 wt. %, but if it is added in too large an amount, there
is the possibility that large TiN inclusion will be produced and become origins of
fatigue breakdown, so the upper limit was set at 0.050 wt. %.
[0019] Boron: Boron strengthens the grain boundary by segregating near the austenite grain
boundary. At less than 0.0005 wt. %, its effect cannot be fully anticipated, but exceeding
0.0060 wt. % will provide no further benefit, and the steel will be more brittle,
so the upper limit was set at 0.0060 wt. %.
[0020] Phosphorus: Phosphorus is an element that lowers the impact value by segregation
at the austenite grain boundary, which makes the grain boundary brittle. This problem
is pronounced when the phosphorous content is over 0.010 wt. %.
[0021] Sulfur: In steel, sulfur is present as an MnS inclusion, and is a cause of shortened
fatigue life. Therefore, to reduce inclusions, the upper limit must be set at 0.010
wt. %.
[0022] O
T: This is the total amount of oxygen as oxide inclusions. If a large quantity of oxygen
is contained, there will be many oxide inclusions that will become origins of fatigue
fracture, so the content should be as low as possible, and the upper limit is 0.0015
wt. %.
BRIEF DESCRIPTION OF THE DRAWINGS
[0023]
Fig. 1 is a graph of the relation between the oxygen content and the rotating bending
fatigue limit; and
Fig. 2 illustrates the shape of the rotating bending fatigue test piece.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0024] The present invention will now be described in further detail through specific examples.
Table 1 shows the chemical components of the developed steels of the present invention
and comparative and conventional steels melted in a large-scale furnace.

[0025] Table 1 shows the impact value and hardness of each sample upon tempered at 350°C
after quenching. In every case the developed steel (marked " A" ) of the present invention
had a hardness Hv of at least 600 and an impact value of at least 40 J/cm
2, but the impact value of the conventional steel (" C" ) and comparative steel ("
B" ) did not reach 40 J/cm
2 even when the hardness Hv was more than 600.
[0026] The present invention is the result of discovering that the oxygen content greatly
affects the characteristics of steel, and to test this, alloys of the composition
shown in Table 2 were used to conduct a mechanical strength and Ono-type rotating
bending fatigue test. These results are also given in Table 2.

[0027] Figure 1 shows the relation between the oxygen content and the rotating bending fatigue
limit. Figure 2 illustrates the shape of the rotary bending fatigue test piece and
the dimensions of the test piece are shown in millimeter units. It was discovered
that an oxygen content of 0.0015 wt. % serves as a boundary, above and below which
there is a clear difference in the fatigue limit, so the upper limit of the oxygen
content was set to 0.0015 wt. % in the present invention.
[0028] Test steels #1 to #4 arbitrarily selected from inventive steels and conventional
steels, respectively, were tested for durability in a coil spring having the spring
characteristics shown in Table 3. The durability test results are given in Table 4.
Two types of durability test were conducted under stress conditions of (A) 100 to
1300 MPa and (B) 500 to 1300 MPa. In table 4, "40.0 halted" means that the test steel
could endure even at the durability test of 40.0x10
4 cycles without breakage and the durability test was halted at this point. The test
results other than "40.0 halted" means that the test steels were broken at the cycles
shown in Table 4.
Table 3
Wire diameter (mm) |
11.5 |
Average coil diameter (mm) |
115.0 |
Effective number of coils |
4.3 |
Total number of coils |
5.5 |
Free height (mm) |
307.6 |
Spring coefficient (N/mm) |
26.17 |
Table 4
Stress conditions (MPa) |
Durability test cycles (× 104) |
|
|
Present invention steel |
Conventional steel |
A |
100-300 |
#1 15.6 broke |
#1 5.1 broke |
#2 12.1 broke |
#2 4.7 broke |
#3 17.2 broke |
#3 8.5 broke |
#4 10.2 broke |
#4 4.9 broke |
B |
500-1300 |
#1 40.0 halted |
#1 12.7 broke |
#2 40.0 halted |
#2 15.3 broke |
#3 40.0 halted |
#3 12.5 broke |
#4 40.0 halted |
#4 13.2 broke |
Hardness (Hv) |
620-628 |
523-531 |
[0029] As is clear from the results in Table 4 above, the service life was greatly extended
compared to the conventional steel under the A conditions, in which the stress amplitude
was large, and a service life of over 400,000 cycles was obtained under the B conditions,
in which the stress amplitude was relatively small.
[0030] The present invention yields a high-strength spring steel whose hardness and toughness
are both better that those of existing spring steel.